Author: Vearl N. HuffPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 22
Book Description
Theoretical Rocket Performance of JP-4 Fuel with Mixtures of Liquid Ozone and Fluorine
Author: Vearl N. HuffPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 22
Book Description
Theoretical Rocket Performance of JP-4 Fuel with Mixtures of Liquid Ozone and Fluorine
Author: Vearl N. HuffPublisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 22
Book Description
Data were estimated by means of a heat correction equation using data for JP-4 fuel with mixtures of oxygen and fluorine. The estimated data were checked for several cases by direct calculations. The difference in specific impulse between the estimated and directly calculated values was from 0.2 to 0.8 pound-second per pound. The maximum value of specific impulse was 334.9 pound-seconds per pound for a combustion-chamber pressure of 600 pounds per square inch absolute and an exit pressure of 1 atmosphere.
Theoretical Performance of JP-4 Fuel with a 70-percent-fluorine - 30-percent Oxygen as a Rocket Propellant
Author: Sanford GordonPublisher:
ISBN:
Category : Fluorine
Languages : en
Pages : 46
Book Description
Theoretical Maximum Performance of Liquid Fluorine-liquid Oxygen Mixture with JP-4 Fuel as Rocket Propellants
Author: Sanford GordonResearch Memorandum
Author: Index of NACA Technical Publications
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860
Book Description
NACA Research Memorandum
Author: Theoretical Performance of JP-4 Fuel with a 70-percent-fluorine-30-percent-oxygen Mixture and a Rocket Propellant
Author: Sanford GordonHandling and Use of Fluorine and Fluorine-oxygen Mixtures in Rocket Systems
Author: Harold W. SchmidtPublisher:
ISBN:
Category : Fluorine
Languages : en
Pages : 292
Book Description
Author: